CN104471195B - 从复合材料制造涡轮机组壳体的方法和相关的壳体 - Google Patents

从复合材料制造涡轮机组壳体的方法和相关的壳体 Download PDF

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Publication number
CN104471195B
CN104471195B CN201380037741.0A CN201380037741A CN104471195B CN 104471195 B CN104471195 B CN 104471195B CN 201380037741 A CN201380037741 A CN 201380037741A CN 104471195 B CN104471195 B CN 104471195B
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CN
China
Prior art keywords
protective layer
flange
mandrel
housing
corrosion
Prior art date
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Application number
CN201380037741.0A
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English (en)
Chinese (zh)
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CN104471195A (zh
Inventor
西尔维·卡拉蒂尼
蒂莫西·伊利瑟夫
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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Publication date
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Publication of CN104471195A publication Critical patent/CN104471195A/zh
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/302—Details of the edges of fibre composites, e.g. edge finishing or means to avoid delamination
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/541—Positioning reinforcements in a mould, e.g. using clamping means for the reinforcement
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2309/00—Use of inorganic materials not provided for in groups B29K2303/00 - B29K2307/00, as reinforcement
    • B29K2309/08—Glass
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/005—Selecting particular materials
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/30—Manufacture with deposition of material
    • F05D2230/31—Layer deposition
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/11—Shroud seal segments
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/95—Preventing corrosion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/601—Fabrics
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • F05D2300/6032—Metal matrix composites [MMC]

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • General Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Moulding By Coating Moulds (AREA)
CN201380037741.0A 2012-07-16 2013-07-08 从复合材料制造涡轮机组壳体的方法和相关的壳体 Active CN104471195B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1256850 2012-07-16
FR1256850A FR2993317B1 (fr) 2012-07-16 2012-07-16 Carter de turbomachine dans un materiau composite et procede de fabrication associe
PCT/FR2013/051626 WO2014013161A1 (fr) 2012-07-16 2013-07-08 Procédé de fabrication d'un carter de turbomachine dans un matériau composite et carter associé

Publications (2)

Publication Number Publication Date
CN104471195A CN104471195A (zh) 2015-03-25
CN104471195B true CN104471195B (zh) 2016-08-17

Family

ID=47553188

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201380037741.0A Active CN104471195B (zh) 2012-07-16 2013-07-08 从复合材料制造涡轮机组壳体的方法和相关的壳体

Country Status (9)

Country Link
US (1) US9909447B2 (enExample)
EP (1) EP2872746B1 (enExample)
JP (1) JP2015524757A (enExample)
CN (1) CN104471195B (enExample)
BR (1) BR112015001033B1 (enExample)
CA (1) CA2879052C (enExample)
FR (1) FR2993317B1 (enExample)
RU (1) RU2637282C2 (enExample)
WO (1) WO2014013161A1 (enExample)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10392950B2 (en) * 2015-05-07 2019-08-27 General Electric Company Turbine band anti-chording flanges
EP3311031B1 (en) * 2015-06-18 2026-02-25 Nuovo Pignone Tecnologie - S.r.l. Casing for a turbomachine
WO2017181087A1 (en) 2016-04-15 2017-10-19 Felicitex Therapeutics, Inc. Combinations for the treatment of neoplasms using quiescent cell targeting and inhibitors of mitosis
CN107399091B (zh) * 2017-07-11 2019-09-06 北京汽车集团有限公司 异形复合材料轴、其制备方法以及与金属法兰的连接方法
FR3074088B1 (fr) * 2017-11-30 2021-02-12 Safran Aircraft Engines Carter en materiau composite renforce et son procede de fabrication
FR3100561B1 (fr) * 2019-09-10 2023-01-20 Safran Aircraft Engines Fixation d’une virole acoustique a une enveloppe de carter pour une turbomachine d’aeronef
FR3105076B1 (fr) * 2019-12-23 2023-04-14 Safran Aircraft Engines Procede de fabrication d’un carter pour une turbomachine d’aeronef
CN117445243A (zh) * 2023-12-21 2024-01-26 浙江航引新材料科技有限公司 一种法兰纤维预制体及其制备方法

Citations (3)

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Publication number Priority date Publication date Assignee Title
EP1674671A2 (en) * 2004-12-23 2006-06-28 General Electric Company Composite fan containment case for turbine engines
CN101249725A (zh) * 2007-02-23 2008-08-27 斯奈克玛 由复合材料制造燃气涡轮机壳体的方法,及由此获得的壳体
US20120076647A1 (en) * 2010-09-28 2012-03-29 Robertson Jr Thomas J Metallic radius block for composite flange

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KR200181300Y1 (ko) * 1999-12-13 2000-05-15 포항종합제철주식회사 플랜지 이음에 있어서 갈바닉 부식 방지 장치
FR2869074B1 (fr) * 2004-04-14 2006-07-21 Snecma Moteurs Sa Systeme de protection d'arbre principal de moteur a palier fusible
US7431978B2 (en) * 2004-12-22 2008-10-07 General Electric Company Reinforced matrix composite containment duct
US7429165B2 (en) * 2006-06-14 2008-09-30 General Electric Company Hybrid blade for a steam turbine
DE102006041321A1 (de) * 2006-09-01 2008-03-06 Rolls-Royce Deutschland Ltd & Co Kg Gehäuseabschnitt, insbesondere Fangehäuse, für ein Gasturbinentriebwerk
US7713021B2 (en) * 2006-12-13 2010-05-11 General Electric Company Fan containment casings and methods of manufacture
US20080157418A1 (en) * 2006-12-27 2008-07-03 Lee Alan Blanton Methods for fabricating composite structures with flanges having tethered corners
US9032706B2 (en) * 2008-09-26 2015-05-19 Pratt & Whitney Canada Corp. Composite fan case with integral containment zone
US8672609B2 (en) * 2009-08-31 2014-03-18 United Technologies Corporation Composite fan containment case assembly
FR2966508B1 (fr) * 2010-10-22 2015-04-03 Snecma Carter de soufflante de moteur aeronautique en materiau composite et procede pour sa fabrication

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1674671A2 (en) * 2004-12-23 2006-06-28 General Electric Company Composite fan containment case for turbine engines
CN101249725A (zh) * 2007-02-23 2008-08-27 斯奈克玛 由复合材料制造燃气涡轮机壳体的方法,及由此获得的壳体
US20120076647A1 (en) * 2010-09-28 2012-03-29 Robertson Jr Thomas J Metallic radius block for composite flange

Also Published As

Publication number Publication date
FR2993317A1 (fr) 2014-01-17
BR112015001033A2 (pt) 2017-06-27
EP2872746A1 (fr) 2015-05-20
FR2993317B1 (fr) 2014-08-15
RU2015104986A (ru) 2016-09-10
WO2014013161A1 (fr) 2014-01-23
JP2015524757A (ja) 2015-08-27
US9909447B2 (en) 2018-03-06
BR112015001033B1 (pt) 2021-11-30
RU2637282C2 (ru) 2017-12-01
US20150192032A1 (en) 2015-07-09
CN104471195A (zh) 2015-03-25
EP2872746B1 (fr) 2018-12-26
CA2879052C (fr) 2020-04-14
CA2879052A1 (fr) 2014-01-23

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